EP2977713B8 - Fuselage nose cap for a missile - Google Patents

Fuselage nose cap for a missile Download PDF

Info

Publication number
EP2977713B8
EP2977713B8 EP15001997.4A EP15001997A EP2977713B8 EP 2977713 B8 EP2977713 B8 EP 2977713B8 EP 15001997 A EP15001997 A EP 15001997A EP 2977713 B8 EP2977713 B8 EP 2977713B8
Authority
EP
European Patent Office
Prior art keywords
missile
nose cap
fuselage nose
fuselage
cap
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
EP15001997.4A
Other languages
German (de)
French (fr)
Other versions
EP2977713B1 (en
EP2977713A1 (en
Inventor
Klaus Bär
Michael Biedermann
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Diehl Defence GmbH and Co KG
Original Assignee
Diehl Defence GmbH and Co KG
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Diehl Defence GmbH and Co KG filed Critical Diehl Defence GmbH and Co KG
Publication of EP2977713A1 publication Critical patent/EP2977713A1/en
Publication of EP2977713B1 publication Critical patent/EP2977713B1/en
Application granted granted Critical
Publication of EP2977713B8 publication Critical patent/EP2977713B8/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/36—Means for interconnecting rocket-motor and body section; Multi-stage connectors; Disconnecting means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/38—Range-increasing arrangements
    • F42B10/42—Streamlined projectiles
    • F42B10/46—Streamlined nose cones; Windshields; Radomes

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
EP15001997.4A 2014-07-23 2015-07-04 Fuselage nose cap for a missile Active EP2977713B8 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102014011035.4A DE102014011035A1 (en) 2014-07-23 2014-07-23 Hull hood for a missile

Publications (3)

Publication Number Publication Date
EP2977713A1 EP2977713A1 (en) 2016-01-27
EP2977713B1 EP2977713B1 (en) 2017-03-01
EP2977713B8 true EP2977713B8 (en) 2017-05-31

Family

ID=53540562

Family Applications (1)

Application Number Title Priority Date Filing Date
EP15001997.4A Active EP2977713B8 (en) 2014-07-23 2015-07-04 Fuselage nose cap for a missile

Country Status (2)

Country Link
EP (1) EP2977713B8 (en)
DE (1) DE102014011035A1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108801078B (en) * 2018-08-23 2024-02-27 中国工程物理研究院总体工程研究所 Explosion-proof rocket projectile
CN110274525B (en) * 2019-06-25 2022-10-04 石家庄市居高科技有限公司 High-speed aircraft with resistance reduction and range extension functions

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3070018A (en) * 1961-02-27 1962-12-25 Marcellus W Fahi Nose cone ejection system
DE7416014U (en) * 1974-05-08 1987-07-02 Dynamit Nobel Ag, 5210 Troisdorf, De
EP0072049B1 (en) * 1981-08-05 1985-09-18 Werkzeugmaschinenfabrik Oerlikon-Bührle AG Process to fasten a ballistic cover to a projectile
DE3802002A1 (en) * 1988-01-25 1989-08-10 Kaltmann Hans Joachim Projectile without any detonator or explosive, for weapons with barrels
US7082878B2 (en) * 2003-07-01 2006-08-01 Raytheon Company Missile with multiple nosecones
DE102005030090B4 (en) * 2005-06-27 2007-03-22 Diehl Bgt Defence Gmbh & Co. Kg Throw-off hood and missile with detachable hood
IL189089A0 (en) * 2008-01-28 2008-08-07 Rafael Advanced Defense Sys Apparatus and method for splitting and removing a shroud from an airborne vehicle
DE102010007064B4 (en) 2010-02-06 2012-03-29 Diehl Bgt Defence Gmbh & Co. Kg Missile head and method of separating a hood from a missile body
FR2960055B1 (en) * 2010-05-12 2015-11-20 Tda Armements Sas GUIDED MUNITION PROTECTED BY AERODYNAMIC COIFFE
US8931738B2 (en) * 2012-02-21 2015-01-13 Raytheon Company Releasable radome cover

Also Published As

Publication number Publication date
EP2977713B1 (en) 2017-03-01
EP2977713A1 (en) 2016-01-27
DE102014011035A1 (en) 2016-01-28

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